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An Investigation of the Low-speed Static Stability Characteristics of Complete Models Having Sweptback and Sweptforward WingsAn investigation has been conducted in the Langley 300 MPH 7- by 10-foot tunnel to determine the static stability characteristics at low speeds of complete models with various swept wings so that comparisons might be made with available theoretical and empirical methods of predicting the stability characteristics. Longitudinal and lateral stability characteristics, flaps up and down, were obtained for models having 0 degree, 15 degrees, 30 degrees, and 45 degrees sweptforward and sweptback wings.
Document ID
19930085510
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Spearman, M Leroy
Comisarow, Paul
Date Acquired
August 16, 2013
Publication Date
November 19, 1948
Report/Patent Number
NACA-RM-L8H31
Accession Number
93R14800
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SWEEP - COMPLETE WINGS
STABILITY, LONGITUDINAL - STATIC
STABILITY, DIRECTIONAL - STATIC
TAIL?WING AND FUSELAGE COMBINATIONS - AIRPLANES
STABILITY, LATERAL - STATIC
FLAPS - COMPLETE WINGS

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